| 基于半导体制冷的某型发射箱温控系统设计 |
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| 引用本文： | 张志利,侯传勋,姜毅,齐月静.基于半导体制冷的某型发射箱温控系统设计[J].弹箭与制导学报,2011,31(1):231-236. |
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| 作者姓名： | 张志利 侯传勋 姜毅 齐月静 |
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| 作者单位： | 张志利,ZHANG Zhili(第二炮兵工程学院兵器发射理论与技术国家重点学科实验室,西安,710025);侯传勋,HOU Chuanxun(第二炮兵工程学院兵器发射理论与技术国家重点学科实验室,西安,710025;中国科学院光电研究院,北京,100190);姜毅,JIANG Yi(北京理工大学宇航学院,北京,100081);齐月静,QI Yuejing(中国科学院光电研究院,北京,100190) |
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| 摘 要： | 阐述了发射箱温控系统设计中保温层厚度、冷热负荷、制冷制热量和相应电源功率的计算步骤,提出了一种基于工况和查表的半导体制冷量快速估算方法。给出了系统软硬件设计,运用单向温度控制、温度偏差梯度控制和PID控制等方法,探讨了适用于多传感器和多热泵交错阵列式分布调温系统的控制策略。测试表明系统在控制精度、温度均布性、能耗效率和自动化程度等方面优于已有装备,对延长待机时间和优化箱体内环境控制有积极意义。
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| 关 键 词： | 温控系统 半导体制冷 控制策略 PWM电源 PID控制 LabVIEW |
Temperature Control System Design for a Certain Missile Launch Canister Based on Semiconductor Refrigeration |
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| ZHANG Zhili,HOU Chuanxun,JIANG Yi,QI Yuejing.Temperature Control System Design for a Certain Missile Launch Canister Based on Semiconductor Refrigeration[J].Journal of Projectiles Rockets Missiles and Guidance,2011,31(1):231-236. |
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| Authors: | ZHANG Zhili HOU Chuanxun JIANG Yi QI Yuejing |
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| Affiliation: | ZHANG Zhili1,HOU Chuanxun1,2,JIANG Yi2,QI Yuejing3(1 State Key Subject Laboratory of Weapon Launching Theory and Technology,The Second Artillery Engineering College,Xi'an 710025,China,2 School of Aerospace Engineering,Beijing Institute of Technology,Beijing 100081,3 Academy of Opto-electronics,Chinese Academy of Sciences,Beijing 100190,China) |
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| Abstract: | The procedures of calculating thermal-insulation-layer thickness,hot and cold load,semiconductor cooling and heating capacity and corresponding electric power which were involved in designing temperature control system for missile launch canister were analyzed.A rapid method based on working condition and looking-up table for estimating the semiconductor cooling capacity was proposed.The system hardware and software design was also discussed,and a new temperature control strategy for systems with multi temp... |
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| Keywords: | LabVIEW |
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